Airbus H225 Super Puma vs. Mil Mi-26
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Airbus H225 Super Puma |
versus |
Mil Mi-26 |
14.06 m |
46 ft 2 in |
length |
40.03 m |
131.3 ft |
4.38 m |
14 ft 4 in |
height |
8.15 m |
26.7 ft |
|
|
wingspan |
|
|
2 x Turbomeca Makila 2A turboshaft engines |
engines |
2 x Lotarev D-136 turboshaft engines |
2,778 hp |
thrust per engine |
8,380 kW |
5,556 hp |
total thrust |
16,760 kW |
11,000 kg |
24,251 lb |
MTOW |
56,000 kg |
123,459 lb |
857 km |
463 nm |
range |
800 km |
432 nm |
242 km/h |
150 mph |
cruise speed |
255 km/h |
158 mph |
24-28 |
capacity |
Up to 90 passengers |
16.2 m |
53 ft 2 in |
rotor diameter |
32.00 m |
105 ft 0 in |
10.7 m/s |
2,106 ft/min |
rate of climb |
8 m/s |
1,574 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.